STC SA00232WI-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00232WI-D This certificate issued to: Rockwell Collins, Inc.

400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Certifies that the change in the type design for the following product with the limitutions and conditions therefer as specified hereen meets the airworthiness requirenents of Purt 23 of the Federal Aviation

• Regulutions, and Special Conditions 23-ACE-68.

Original Product - Type Testificate Number: A24CE Abuke: Raytheon (Beech) Model: A200CT (C-12F or C-12D), B200C (C-12F) Description of Type Design Change: Installation of Collins FDS-255 Flight Display System. See TABLE 1 or TABLE 2 or TABLE 3 on Sheet 2, or TABLE 4 or TABLE 5 or TABLE 6 on Sheet 3, or TABLE 7 on Sheet 4.

Limitations and Conditions: (1) Compatibility of this design change with previously approved modifications must be determined by the installer. (2) This STC must be installed concurrently with STCs SA00234WI-D (Drawing Index AAC-0250-001), SA01037WI-D, SA01038WI-D and SA01039WI-D. (3) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Administruter of the Federal Aviation Administration .

Date of Application: February 21, 1997 Dutt reisined:

Lete of instance: October 31, 1997 Lute umended: November 24, 1997, February 3, 1998 December 20, 2001, September 24, 2003, April 18, 2005, March 20, 2006, EDERAL AVIATION April 3, 2006 By Direction of the Administrator ADMINIS RATION A John S. Bohn an A Been (Signature) Administrator, DAS-500864-CE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00232W-D (Continued) TABLE 1 C-12F(F1) TO (T1 AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplemen Index Configuration (AFMS) (MMS) AAC-0021-001, Collins FDS-255 Flight Display System AAC-0040, AAC-0039, No revision, in Beech A200CT No revision, No revision, dated 4/8/97 dated 10/9/97 dated 10/9/97 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

TABLE 2 C-12F(F2) TO (T2 AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplemen Index Configuration (AEMS) (MMS) AAC-0027-001, Collins FDS-255 Flight Display System AAC-0040, AAC-0039, No revision, in Beech B200C Revision A, Revision A, dated 10/15/97 dated 11/24/97 dated 11/24/97 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

TABLE 3 C-12F(F3) TO (T3 AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplemen Index Configuration (AFMS) (MMS) AAC-0030-001, Collins FDS-255 Flight Display System (4 tube) AAC-0040, AAC-0039, No revision, in Beech B200C Revision B, Revision B, dated 12/19/97 dated 2/3/98 dated 2/3/98 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

FAA FORM 9110-2-1(10-69) PAGE 2 of 4 PAGES

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00232WI-D (Continued) TABLE 4 C-12F(F3 OR T3) TO (U AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplemen Index Configuration (AFMS) (MMS) AAC-0251-001, Collins FDS-255 Flight Display System (5 tube) AAC-0247, AAC-0290, No revision, in Beech B200C No revision, No revision, dated 10/23/01 dated 12/20/01 dated 12/20/01 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

TABLE 5 C-12F(F1 OR T1) TO (U AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplemen Index Configuration (AFMS) (MMS) AAC-0318-001, Collins FDS-255 Flight Display System (5 tube) AAC-8085, AAC-8090, No revision, in Beech A200CT No revision, No revision, dated 02/25/03 dated 09/24/03 dated 09/24/03 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

TABLE 6 C-12D(D2) TO (U AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplemen Index Configuration (AEMS) (MMS) RCA-0087-001, Collins FDS-255 Flight Display System (5 tube) AAC-0398, AAC-8108, No revision, in Beech A200CT No revision, No revision, dated 03/21/05 Dated 04/04/05 dated 04/18/05 or later FAA Approved revisions to the Drawing Index, AFMS and MMS.

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00232W1-D (Continued) TABLE 7 C-12F(F2 OR T2) TO (U AVIONICS CONFIGURATION) Collins Airplane Flight Maintenance Drawing Manual Supplement Manual Supplemen Index Configuration (AFMS) (MMS) AAC-0338-001, Collins FDS-255 Flight Display System (5 tube) AAC-8100, AAC-8095, Revision A, in Beech B200C No revision, No revision, dated 04/03/06 dated 03/20/06 dated 03/20/06 or later FAA Approved revisions to the Drawing index, AFMS and MMS.

FAA FORM 8110-2- 1(10-69) PAGE 4 of 4 PAGES